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You searched for: subject:"Aerofoils"
[texts]Wing theory - Robinson, Abraham
http://uf.catalog.fcla.edu/uf.jsp?st=UF023772925&ix=pm&I=0&V=D&pm=1
Keywords: Aerofoils
Downloads: 139
[texts]Present state of development in nonsteady motion of a lifting surface : = Lo stato attuale delle ricerche sul moto instazionario di una superficie portante - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003689766&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Aerofoils
Downloads: 92
[texts]Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779967&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Aerofoils
Downloads: 139
[texts]Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 651-210 airfoil section - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003600239&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 70
[texts]On the design of airfoils in which the transition of the boundary layer is delayed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778659&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar flow; Aerofoils
Downloads: 126
[texts]Completed tabulation in the United States of tests of 24 airfoils at high Mach numbers: (derived from interrupted work at Guidonia, Italy in the 1.31- by 1.74-foot high-speed tunnel - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605300&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Wind tunnels
Downloads: 121
[texts]Development of a real-time hybrid computer simulation for the 3K-SES, 5 DOF, data-based program : part I: familiarization and planning - Gerba, Alex.;Thaler, George J.
Progress report period ending June 1979--Cover.
Keywords: AEROFOILS; UNSTEADY FLOW (AERODYNAMICS)
Downloads: 64
[texts]Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614876&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Compressibility; Aerodynamics--Research
Downloads: 104
[texts]Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 652-415, 653-418 and 654-421 airfoil sections - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806709&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 160
[texts]Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter) : = Profilmessungen im DVL-Hochgeschwindigkeitswindkanal (2,7-meter Durchmesser) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003690341&ix=nu&I=0&V=D&pm=1
Keywords: Camber (Aerofoils; Aeronautics
Downloads: 88
[texts]Effect of compressibility on the pressures and forces acting on a modified NACA 65,3-019 airfoil having a 0.20-chord flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638549&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Compressibility; Aerodynamics--Research
Downloads: 97
[texts]Circulation control airfoil study : progress report no 4 - Schmidt, Louis Vincent
Title from cover
Keywords: Aerofoils; Unsteady flow (Aerodynamics)
Downloads: 62
[texts]Die aeroplane und luftschrauben der statischen und dynamischen luftschiffahrt schwerer und leichter als luft - Dallwitz-Wegner, Richard von, 1873- [from old catalog]
Book digitized by Google and uploaded to the Internet Archive by user tpb.
Keywords: Aerodynamics; Aerofoils; Propellers, Aerial
Downloads: 141
[texts]Airfoil theory at supersonic speed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780837&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Aerofoils
Downloads: 245
[texts]Profile-drag coefficients of conventional and low-drag airfoils as obtained in flight - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605308&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aeronautics--Research
Downloads: 95
[texts]Airfoil-contour modifications based on [epsilon]-curve method of calculating pressure distribution - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003609112&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 68
[texts]Wind-tunnel investigation of control-surface characteristics.: XVI,Pressure distribution over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge flaps - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804344&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamic load
Downloads: 120
[texts]Resistance of cascade of airfoils in gas stream at subsonic velocity - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779974&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics; Laminar boundary layer
Downloads: 91
[texts]Conformal transformation of an airfoil into a straight line and its application to the inverse problem of airfoil theory - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614298&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Transformations (Mathematics; Aerodynamics--Research
Downloads: 142
[texts]Scale-effect tests in a turbulent tunnel of the NACA 653-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613066&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerofoils; Aerodynamics--Research
Downloads: 75
[texts]Wind-tunnel investigation of NACA 66(215)-216, 66,1-212, and 651-212 airfoils with 0.20-airfoil-chord split flaps - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003622093&ix=nu&I=0&V=D&pm=1
Keywords: Flaps (Airplanes; Aerofoils; Aerodynamics--Research
Downloads: 104
[texts]Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638560&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Aerofoils; Aerodynamics--Research
Downloads: 87
[texts]Effects of specific types of surface roughness on boundary-layer transition - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616147&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Reynolds number; Aerodynamics--Research
Downloads: 117
[texts]Scale and turbulence effects on the lift and drag characteristics of the NACA 653-418, a = 1.0 airfoil section - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605349&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerofoils; Aerodynamics--Research
Downloads: 129
[texts]Airfoil interaction with an impinging vortex - McAlister, Kenneth W
Distributed to depository libraries in microfiche
Keywords: Vortex-motion; Aerofoils; Stalling (Aerodynamics)
Downloads: 230
[texts]Wind-tunnel investigation of control-surface characteristics.: XXI,Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.40-Airfoil-Chord flap on an NACA 0009 airfoil - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807479&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerofoils; Aerodynamics--Research
Downloads: 100
[texts]Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613553&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Control surfaces; Aerofoils; Aerodynamics--Research
Downloads: 91
[texts]Effects of roughness at high Reynolds numbers on the lift and drag characteristics of three thick airfoils - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614465&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerofoils; Lift (Aerodynamics; Aerodynamics--Research
Downloads: 171
[texts]Discrete time series generated by mixtures III : autoregressive processes (DAR(p)) - Jacobs, Patricia A.Lewis, Peter A. W.
Title from cover
Keywords: AEROFOILS.JET FLAPS (AIRPLANES); LEADING EDGES (AERODYNAMICS)
Downloads: 98
[texts]Aerodynamic tests of an AN-M-65-AZON 1000-pound radio-controlled bomb in the LMAL 16-foot high-speed tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003612700%26ix=nu%26I=0%26V=D%26pm=1
Keywords: Aerofoils; Mach number; Guided bombs; Aerodynamics--Research; Aerodynamics--Research
Downloads: 103
[texts]Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638506%26ix=nu%26I=0%26V=D%26pm=1
Keywords: Mach number; Aerofoils; Drag (Aerodynamics; Lift (Aerodynamics; Aerodynamics--Research; Aerodynamics--Research
Downloads: 475
[texts]Flow field measuremnts of an airfoil with deflected spoiler using a two-component LDV sys - Foreman, Michael J.
"NPS-67-86-008."
Keywords: Aeronautics; Aerofoils; Spoilers (Airplanes); Laser Doppler velocimeter; Airplanes; Control surfaces; Fluid dynamic measurements
Downloads: 61
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